US Patent No: 8,181,913
Number of patents in Portfolio can not be more than 2000
Slat support funk plate
Stats
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May 22, 2012
Issued date -
Oct 7, 2008
filing date -
12/246,816
serial no -
In Force
status
Importance
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Abstract
An aircraft wing high lift assembly comprising a movable element and a load receiving element including a body portion having a first load receiving region arranged to receive loads from the movable element in a first direction during normal operation of the high lift assembly and including at least one restraining arm projecting from the body portion, the or each restraining arm having a second load receiving region arranged to receive loads from the movable element in a second direction in the event of a failure within the high lift assembly.
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First Claim
Related Publications
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International Classification(s)
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Cited Art
| Patent Info | (Count) | # Cites | Year |
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| 4,360,176 Wing leading edge slat | 42 | 1979 | |
| 4,399,970 Wing leading edge slat | 27 | 1980 | |
| 4,471,928 Extendible airfoil track assembly | 13 | 1982 | |
| 4,475,702 Variable camber leading edge assembly for an airfoil | 48 | 1982 | |
| 4,615,499 Wing slat anti-ice air duct system | 16 | 1983 | |
| 4,706,913 Variable camber leading edge assembly for an airfoil | 42 | 1984 | |
| 4,640,477 Closing device for an airfoil | 7 | 1984 | |
| 4,650,140 Wind edge movable airfoil having variable camber | 43 | 1985 | |
| 4,753,402 Biased leading edge slat apparatus | 11 | 1985 | |
| 5,158,252 Three-position variable camber Krueger leading edge flap | 47 | 1991 | |
| 5,544,847 Leading edge slat/wing combination | 41 | 1993 | |
| 5,628,477 Auxiliary airfoil lost motion detector and actuator | 21 | 1995 | |
| 5,681,013 Vortex leading edge flap assembly for supersonic airplanes | 10 | 1995 | |
| 5,927,656 Wing leading edge flap and method therefor | 45 | 1996 | |
| 5,839,699 Leading edge slat/wing combination | 16 | 1996 | |
| 2011/0024,575 LEADING EDGE FLAP METHOD | 3 | 2010 | |
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| 6,149,105 Deployment mechanisms for aircraft auxiliary airfoils | 5 | 1996 | |
| 2010/0187,368 ACTUATION SYSTEM FOR LEADING EDGE HIGH-LIFT DEVICE | 1 | 2008 | |
| 2011/0168,849 SLAT SUPPORT ASSEMBLY | 2 | 2009 | |
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| 4,838,503 Mechanism for supporting and extending a high lift device for aircraft wings | 30 | 1988 | |
| 5,044,580 Flexible closing device for a wing leading edge | 4 | 1990 | |
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| 2011/0011,984 High Lift System for an Aircraft | 1 | 2008 | |
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| 4,880,189 Device for closing and opening in the leading edge of a wing | 6 | 1988 | |
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| 2010/0163,685 WING | 1 | 2008 | |
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| 6,457,680 Auxiliary airfoil for aircraft main wings | 10 | 2000 | |
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| 4,470,569 Locking, redundant slat drive mechanism | 20 | 1981 | |
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| 5,094,412 Flaperon system for tilt rotor wings | 48 | 1989 | |
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| 2002/0027,612 Spatio-temporal channel for images | 3 | 2001 | |
Patent Citation Ranking
Maintenance Fees
| Fee | Large entity fee | small entity fee | micro entity fee | due date |
|---|---|---|---|---|
| 3.5 Year Payment | $1600.00 | $800.00 | $400.00 | Nov 22, 2015 |
| 7.5 Year Payment | $3600.00 | $1800.00 | $900.00 | Nov 22, 2019 |
| 11.5 Year Payment | $7400.00 | $3700.00 | $1850.00 | Nov 22, 2023 |
| Fee | Large entity fee | small entity fee | micro entity fee |
|---|---|---|---|
| Surcharge - 3.5 year - Late payment within 6 months | $160.00 | $80.00 | $40.00 |
| Surcharge - 7.5 year - Late payment within 6 months | $160.00 | $80.00 | $40.00 |
| Surcharge - 11.5 year - Late payment within 6 months | $160.00 | $80.00 | $40.00 |
| Surcharge after expiration - Late payment is unavoidable | $700.00 | $350.00 | $175.00 |
| Surcharge after expiration - Late payment is unintentional | $1,640.00 | $820.00 | $410.00 |